SCIENTIFIC ABSTRACT KOSMODEMKANSKAYA L.T. - KOSMOWSKA, A.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000825120016-6
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: June 14, 2000
• Sequence Number: 16
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

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_KOSM'OD&'4'YANSKAYA, IVUbovl Timofeyevna [R:aj3madSj&_
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varying soil and Climatic conditlons, in only
wing without the moldbaftrd Tesl&t in any increase in
yield; in 26 the e3m~ct YiadimB Obt*iUed as with Ordina-
ry plowing, and in 18 cases there was a significant decli-
ne in yield. When discing was used instead of ordinary
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ted for a;long time gave no increase in yield con1wed
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S/035/62/000/0 121029106PI
A001/A101
AUTHOR: Xosmodemlyansk~.y A
TITLE: The satellite In flight
PERIODICAL: Referativnyy zhurnal, Astronomiya I Geodeziya, nu. 12, 1962, 85.
abstract 12A631 ("Aviatslya I kosmcnavtika", 1962, no. 7, 49 - 53)
TEXT: The classical problem of two bodie*a*is expounded in application to
motion of Earth's artificial satellites.
[Abstracter's note: Complete translation]
Card 1/1

KOS1,1011-111-11Y.WKII, ATIM-My ALEKSANDW-)VICH
Kteorii lobobogo sporotivle niia. Chast'III. 0 vikhrevom soprotivlenii.
llookva, 1935. 18 p., diagrs. (TsaCi. Trudy, no. 216)
Sumnary in English.
Title tr.: Contribution to the drag thoory-4 Part III. Vortex resistance.
QA 9E,1,165 no.216
SO: AERONAUTICAL SCIEFCES AND AVIATION IN THE SOVIET ~JNION, LIBIbUff OF CONGRESS,
1955

Y, t(.-orii lobovora -,oproiOvIen !a. 1. Priblizhennm-
critsiallriogo ura-monlia larfdriarno *f-o pof.,rbnichnoj~o sdoiza. :]'IL I., ITrutly,
1935, no. 215, P. 3-20, diq!rs.)
,Swviai~%v in Enrlish.
'N tle tr. -. Conlur~bution to drpLr theo-y. 1. I'lletho-6 of ~ntejrra 1401,
U~
of difft-rf~ntial equatimi of .1hc lai,,O.nar boandlary layer.
6
,A911. M 5 no.
Acrotm-LiLical Se-kncr. a~lld Avl:itioa m tlo~ Soviet Union. Librarv of
ConrreFs, 111`5-5.

K teorii lobovorc., so-protivi, niia. 11. T -oreticheskii raschet profill-
nogo soprotivlentia ~idia ZhukovskoCoe Tr-udj, 1~35, no. 215, -p.
21-.-4, diarrs.)
clunim,ar, in A*,'n[-lish.
Title Lr.: Contribution to dra.- thoor7. II. Th(--orctical of
the Profile dra,- of Zhu,-o,,,skji-typc rudder.
-A911. M65 no. 215)
SO. Aeronautical Scj~-nce and Aviation in bhe Soviet Union. Library Of
ConEress, 195:5.

KOSHODEN VNSKIY) ARKADIV ALM, SAITDR-OVTC14
Vikhrevoe soprotivienie teoreticheskikh profilei. Moskva, 1937. 56 p., plates,
diagrs. (TSAGI. Trudy, no. 317)
Title tr.: Eddy resistance of theoretical airfoils,
QA911. ~Z5 no- 317
SO. Aeronautical Science and Aviation in the 3ov-let Union. Library of Congress,
1955.

KOSDIOMPIANSKIJ, ARKADIY ALEKSANDROVICH.
Lobovoe soprotivlenie kryllev S.A. Chaplygina. 'Kryllia tipa inversii elli sa).
1
(Moscow. Universitet. Uchenye zapiski, 1937, no-7-- Plekhanika. p.103-111~
Sunumr-j in French.
Title tr.: Drag of Chaplygin wings. (Wings of the inverted ellipse type.)
Q60JO68 1937, no.7
SO: Aeronautical Sciences and Aviation in the Soviet Union, Library of Congresss
1955.

ARKADIJ ALE-K-SA ~~T!); -VICH.
j- . /~%O U
I
K pro"Aeme vikhrevof.-o soprotivIeniia. (-Mo-;co,,-j. Un-iversitet. Uc'rien.'.,-,
zapiski, 1937. no. 7: IMekhanika. D. 11-1--116)
Sturarar-y in French.
Title- tr.: Tile problem of vortex
1937, no. 7
SO. Aeron.,.,.utical Sci-nee. and Avi,ition in t,lic Snid.rAL, UnJon. Lai-rary of
Congress, 1955-

KOSMODEM ~AMSKI/", A*ADI ALEEKSANDROVICH.
I V
Nekotorye, voprosy acrodinamicheskoi teorii soprot-I leniia. (,oscow. Universitet. Uche-
nye zapiski, 1940, no. 46: Mekhanika, P. 39-83;, illus., diaprs.)
Title tr.: Some Problems of the aerodynamic theroy of drag.
Q60.11866 1940, no. 46
SO: Aeronautical Sciences and Aviation in the Soviet Union, Library of Oongress,
1955

K.03MCDEWYAMM, A.A..
Obahchie teoremy mekhaniki tela peromennoi irmsey
(General theorems of the mechanics of a body of variable mnss), Izd.
VV-TV (Voermo-vozdushnoi inzhenernoi akadendi imenl Zhulovskopo),
MOSCOW) ls)461 16 pp.

KOSMODEMOYANSKIYI A. A.
ItExtremal Problem for a Point of varyl.ng Mass," Dokl. AN SS-IR, 53, No.1, 1946

Ii-TSVIMEMIYATISKIY. A.A.
It.'eldinnika tel peremennol mnss~r; teo -iva reaktivnogo
dvizheniya. (1,11echanics of bodies of variable mass; theory of reactive
notion), Izd. WIA (Voenno-vozd-ashnoi inzhenernio rJmdemii imeni
zhukovaleo6o), Moscow, 110 Pp.

KOSMODEMI~ANSK4, ARKADI~ ALE~MROVICH.
Konstantin Eduardovich TSiolkovskii, 1857-1935; atenogramma
publichnoi lektaiis prochitannoi v Moskve. Moskva., Pravda., 1948.
31 p., illus., port.
Title tr.: Konstantin Eduardovich TSiolkovskii, 1857-1935;
a stenographic report of a public lecture delivered in Moscow.
TL54O.T84K6
SO: Aeronautical Sciences and Aviation in the Soviet Union, Library of
Congress, 1955.

KOSIODEM N SKI IA. A
Ocherki po istorii teoreticheskoi mekhanlIkl v Possli- ('~Os'cow.
liniversitct. Ucheme zapiqM, 1943, no. 122: '-lek-h-Arlika, v. II, p.
193-296)
Title tr.: Historical sketchon of theoretif-al mechinics in Russia.
r,60-M868 191.,8, no. 122.
"10: Aeronautical Sciences Pund Avintlon in thp Soviet Un.;on, Library of
Congress, 1955.

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Acad. Sci., Sect. Toch. phya. (j2), 1872 (t)~ coo
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Mathematical Reviews Kosmodemlyanskii. A. A. General theorems of the ~P-amcs
Vol. 14 No. 10 of a b6dy of variable mais. Mos~-ov, Cos. Univ. Ucenye
Nov. 1953 Zapiski 352, Mehunika 3~ 13-11,12 (1951)i (Russihn)
Mechanic@ This papeir criVers the snang176und hd toctuflis A knd 9 of
thA PhIft- reViewed belcw4 R. A. Hank1h

KOSMb=IYANSX1Y,..A,.A.
Ov
Ul/

iodeni'xans,
'!ZOG? 'dY, A "Lectures oil the mechanics pf
?Ifdr6f7ViffiAbIC mass, Mosicov, Gtog. Uriff, Utellyc
154, Melmii;Pa 4' 7.M80 (1951). =tmsiany
'I'lim lectures are frmn~ a c(purse which the author has

Mathematical Reviews 11 since the session 19b/44 at the Soviet academy of
'pvc
1
Vol. 14 No. 10 m;l4itry and aeronautical coginv-riiq, The paper lx.,gins

Nov
1953 xvith4a historical account of Owlimlical inechanies givin'
9
-
'
eslle6al ellijillasis to tile work 4[
N _(1859-1935) "I'd
Mechanics TsiolkovskiY (
-
- 1357-1935) wh6evidrioly were the firsi t
.
l
i c-o
Mlifer mail elliaticilly problems cfmrvioing bodies,of
VAI'iable mars. Tile work of 1--mmuh-Pulferic, Goddard,
Obert n
li, 1xvi- Civi 0, Tmn (ter and I-Cont I ra ti A is me floned,

4 but t1
icre is no reference to more recent work done outside
Fi0it lecture, Here lie derived the equations of motion
Of a liarticle (tile atithor uses the word"point' for the'Imird

4. 'part~i 41c'-which lie uses in a different connexion) of virl#le
inclilding the equalioll
(IV dAr
T?
whereAlit; the mass of the particle,v itsvelovily, I (lit, time,
Fthe umternal force acting and V, file velocity of
tile ejected rhirt. III tile case when tile atigolme velority of
art is 7,CM this equation wl"A fimm uhtailleMly
~t IL ejected 11,
ImemerskiT [Thesis, St. Petersimirg, 18971. E(jualion (1) is
resolvW into three scalar equations for file caw. m-licii I?
in composed of gravity and air resistance in file direction
~
Se forces are neglected, t lie now
Opposi ng motion. When t hr-
Lv~ll-known law v-vo+V,Iog (AIDIAI) isdilluml fmiliji)
j
-

_A #I S
W6 i I-
I 0--si-ng int'iss aric! gaining all attri The 'bill-flilir
motion' of a particle cl q b6illi'l 6~iid
ma%s is obtained; it is of similar fo n are h)
rm a d was'given by (i) MIA19 I - (ii) f(l)
Mg~crskil [Izvi!stiya St.-Peterburg, Politchn. Inst. I no. Octall.
1-2, 77-118.(t904)], In 12 this is applied, as an 'Sci-ond lecture.-The vertical anovenient of a pailide
approxima- of
tion, to the motion of a reaction boat which expejs the snine variable mass with the 'second burning lair, undera ilitiforin
amount of water as it takes in.The motion of a uniform ficl&of gravity and without air resistance, is considered:
chain falling over the edge of a table i3 studied tlq a further the ifiaxitnuin height 11 attairinble, for given a, V, and final i
ample on varnibl ' mans in �K mass' At., is obtained. It is deduced that 11 is gn~atvst when I
ex, a
irt.,raft i.e., when the mass is tedured from Ho to Al, in.
Fifth lecture. In J~ the rectilineir motion of an a
statilaneou.,41y. The low
with air-jet motor is considered; it is assumed that calldi. ximurn height attainable at file I
tions are such that the rticle theory can fie allplied inatatit of 'all-burnt' iq also -olitained. Rectiliticar inotioll
pa
for example, tile motion of the mass-rentre in tile aircraft without gravity with the first burning law and a
reAstailre.
1 is supposed negligible, and the motion of ilia air inside the Proportional to the square of the velocity is niso considetvd.
- aircraft is -ignored. Resistance is tiken to be proportionni Third lecture. In �1 die. motionunder a resistance of the -
to velocity. The velocity calcu form it+bv is considered for the first burnin '
and horizontal range are g law. In �2 ilia
cousiders a jet aircraft movinj herizantal(y ag, inst
lated. In �2 rectilinear motion of a particle under gravity is autlict
treated for a geri~ral )a_w of air resistance, it being assumed air rwistance so that the lift just com .pIens"Ites tile Weight.
f the The application of the particle theory to this problem is, of
that the rate of gain*
ing mass is.a constant multiple e
rate of Wing mass. The optimum form of the function f (1) coursq1 only possible as an approximation. The distance
is found irk order to give the maximurn'range. in p tile i travelad during the period when the jet is acting is calcu-
lated, for the first burning law, And the optimum value of
similar problem of finding the optimum f(f) such that a
cr is o"ntaincd, In �3 vertical motion under uniform grsvity
given distance is traversed in a minimum time Is discumed mtbj!~ t to air resistance proportional to the velocity is
In both cases /Q) is obt.
iined'Ihi,the first place; as a functio consid .itred. In �4 the problem. is of vtytical motion away
1, of the velocity. from the surface of the earth under varying gravity; ai
ts'dphiv~fth th6 cohvem pmblem' Whe're r
Sixth lectum Thi resistivace. Is negiceted and the mamirnum velocity attnine('
from knowh taternal forces and Motion the I 'aw of burn g Ji ,ffl fly I th t the distance
in. cien smal so a jovrd from the
is to be deterraineO. In 11 -suib.6 problem due to M . mall in comparison with the --. th's radius. ThC.5C
surfaco is 6
ered., it ' asm~' ed t6t s and v ow
(1897) is consid 14 M assumi)tions permit simplifying approximations to be used
nd the Wi
as furic6orill of 1; a1w Stal(s) and the--isid when